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BW-MINS327

By BWSENSING ↗

The BWSENSING BW-MINS327 is a compact micro inertial navigation system for unmanned aircraft, robots, vehicles and stabilized platforms. Its 60 × 59 × 29 mm package provides gyroscope and accelerometer sensing, Kalman filtering and bias tracking, with a 9–36V DC supply and selectable interface outputs.

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Manufacturer and modelBWSENSING BW-MINS327 micro inertial navigation system
Dynamic attitude accuracy0.3°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.1°/60s
Gyroscope resolution0.01°/sec

Product overview

The BWSENSING BW-MINS327 is a packaged micro inertial navigation system intended for unmanned aircraft, robots, platform stabilization and vehicle applications. Its sensing specifications cover a gyroscope and an accelerometer with X, Y and Z axes. Processing features include Kalman filtering and a dedicated bias-tracking algorithm for drift elimination. The packaged unit measures 60 mm long, 59 mm wide and 29 mm high. Electrical integration requires a 9–36V DC supply, with selectable RS232, RS485, TTL and Modbus output options.

The BW-MINS327 specifies dynamic attitude accuracy of 0.3° and static accuracy of 0.01°, with measurement ranges of ±90º in pitch and ±180º in roll. Heading retention accuracy is 0.1°/60s, and accelerometer range is ±1.8 g on all three axes. Operation spans -40℃ to +85℃ with temperature compensation. Accelerometer bias stability is 0.001mg at 25℃, 100s, 1σ, and 0.01mg at 25℃, 10s, 1σ. Gyroscope bias stability across the full temperature range is 15°/h under the stated 10s, 1σ conditions.

Specifications

SpecificationValue & conditions
Manufacturer and modelBWSENSING BW-MINS327 micro inertial navigation system
Dynamic attitude accuracy0.3°
Static attitude accuracy0.01°
Attitude measurement rangePitch ±90º; roll ±180º
Heading retention accuracy0.1°/60s
Gyroscope resolution0.01°/sec
Gyroscope bias stability15°/hFull temperature range; 10s, 1σ.
Angular random walk coefficientLess than 0.1 °/√h
Accelerometer measurement range±1.8 gX, Y and Z axes.
Accelerometer bias stability at 100s0.001mg25℃, 100s, 1σ.
Accelerometer bias stability at 10s0.01mg25℃, 10s, 1σ.
Supply voltage9–36V DC
Interfaces and protocolRS232 / RS485 / TTL / ModbusSelectable output options.
Temperature range-40℃ to +85℃With temperature compensation.
DimensionsL60 × W59 × H29 mmPackaged product.
Bias trackingDedicated bias-tracking algorithm for drift elimination
FilteringHigh-performance Kalman filter algorithm
ApplicationsUnmanned boats and underwater vehicles; robots; platform stabilization; large vessels; automated guided vehicles; automated and driverless operation; special-purpose vehicles; unmanned aircraft
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